• DocumentCode
    2060482
  • Title

    Robust control techniques for adaptive optic space telescopes

  • Author

    Burtz, Major Daniel

  • Author_Institution
    United States Air Force, Nokesville, VA, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    17
  • Abstract
    Future space telescopes will contain lightweight, flexible, segmented mirrors. Traditional control approaches for mirror alignment and shape control may be inadequate due to flexibilities and low natural frequencies. Using adaptive optics for space telescopes presents a possible solution. This research proposes H¿ robust control techniques for these types of systems. An H¿ controller is synthesized for a complex analytical model. This was accomplished with a new technique for model reduction using Zernike polynomials. The H¿ design process used was validated on a simpler adaptive optics testbed. The experimental verification also showed that the robust control techniques outperformed the classical control techniques in the presence of disturbances. The results are a Zernike polynomial method for model reduction, robust controller synthesis for a complex adaptive optics analytical model, and experimental verification on an AO testbed. Although the robust control design is more complex, it provides improved performance in the presence of uncertainty in the disturbances and modeling.
  • Keywords
    adaptive optics; astronomical techniques; astronomical telescopes; robust control; H¿ controller; H¿ design process; Zernike polynomial method; adaptive optic space telescopes; control techniques; mirror alignment; robust control techniques; shape control; Adaptive optics; Analytical models; Frequency; Mirrors; Polynomials; Reduced order systems; Robust control; Shape control; Telescopes; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446713
  • Filename
    5446713